What was found
FOUND CORROSION AT BS1016 BETWEEN S20L-S21L MEASURING .5'X.5' REF: TTG8Q00J55UF<[01] SRM 53-70-01-2R-4 IS FOUND TO BE APPLICABLE;[02] PERFORMED DAMAGE CUTOUT ON FUSELAGE SKIN BS 1016 STR 21L L=3.2'XW=2.9'. IAW SRM 53-70-01-2R-4 STEPS 4.B.(1-2).;[18] INSTALLED 100% PERMANENT AND TEMPORARY FASTENERS PRIOR TO SEALANT SQUEEZE OUT TIME AT 23:00 UTC IAW SRM 53-70-01-2R-4 STEPS 4.L AND SRM 51-40-02.;[19] VERIFIED CORRECTIVE ACTION #18.;[20] INSTALLED 100% OF PERMANENT FASTENERS ON REPAIR PARTS; [1] DOUBLER; [2] STRUCTURAL FILLER AND [3] STRUCTURAL FILLER BETWEEN STR L-20 TO STR L-24 AND BETWEEN BS1006 TO BS1016.APPLIED AERODYNAMIC FILLET SEAL ALL AROUND THE PERIPHERY OF AREA COMMON TO REPAIR; PER SRM 53-70-01-2R-4; REPAIR 4 STEPS L; M; N; O & P.;[21] VERIFIED CORRECTIVE ACTION #20;[22] APPLIED A LAYER OF BMS 3-23; CORROSION INHIBITING COMPOUND TO ALL THE INTERNAL STRUCTURE IN THE REPAIR AREA IAW SRM 53-70-01-2R-4 STEP 4. Q;[23] VERIFIED CORRECTIVE ACTION #22;[24] VERIFIED TASK COMPLETE